IMPREGNATION CLAMPING MANDREL FOR MAKING GAS TURBINE CASINGS MADE OF COMPOSITE MATERIAL
    5.
    发明申请
    IMPREGNATION CLAMPING MANDREL FOR MAKING GAS TURBINE CASINGS MADE OF COMPOSITE MATERIAL 有权
    用于制造复合材料气体涡轮机壳的冲压夹具

    公开(公告)号:US20140283977A1

    公开(公告)日:2014-09-25

    申请号:US14352856

    申请日:2012-10-17

    Applicant: SNECMA

    Abstract: An impregnation mandrel for production of gas turbine casings made from composite material, the mandrel including: an annular wall with a profile of an outer surface that corresponds to that of an internal surface of the casing to be produced; two side plates, with profiles that correspond to those of external casing flanges to be produced; and a removable device for clamping a layer having a fibrous texture, which is wound around the mandrel.

    Abstract translation: 一种用于生产由复合材料制成的燃气轮机壳体的浸渍心轴,所述心轴包括:环形壁,其外表面的轮廓对应于待生产的壳体的内表面; 两个侧板,具有对应于要生产的外壳法兰的轮廓; 以及用于夹紧缠绕在心轴上的具有纤维织构的层的可移除装置。

    Filament wound crew rest enclosure structure
    7.
    发明授权
    Filament wound crew rest enclosure structure 有权
    灯丝伤口人员休息室结构

    公开(公告)号:US07448576B2

    公开(公告)日:2008-11-11

    申请号:US11776134

    申请日:2007-07-11

    Abstract: A mobile platform personnel berth unit and a method for creating the mobile platform personnel berth unit are provided. A male mandrel is created defining an inner mold line surface of the berth unit. The male mandrel is overlayed with one or more layers of filament strips. The filament layers are thermally cured to create an integrated structural member. The male mandrel is then removed from the structural member. The structural member is profile shaped to create a semi-finished berth unit having a top, a bottom and a pair of integral side panels. Additional entrance and back panels as well as access panels and connecting hardware are then added to complete the berth unit.

    Abstract translation: 提供移动平台人员泊位单元和创建移动平台人员泊位单元的方法。 产生一个公心轴,限定了泊位单元的内模线表面。 阳心轴与一层或多层细丝带重叠。 长丝层被热固化以产生一体化结构件。 然后从结构构件中取出阳心轴。 结构构件的轮廓成形以形成具有顶部,底部和一对整体侧板的半成品泊位单元。 然后添加额外的入口和后面板以及检修面板和连接硬件来完成泊位单元。

    Squeeze loops and method for making the same
    8.
    发明申请
    Squeeze loops and method for making the same 审中-公开
    挤压循环和制作相同的方法

    公开(公告)号:US20040238108A1

    公开(公告)日:2004-12-02

    申请号:US10623630

    申请日:2003-07-22

    Abstract: A method for making a squeeze loop includes step of preparing pre-preg yarns and wrapping the yarns to a mandrel; step of solidifying the yarns and removing the mandrel from the yarns which forms a tube; step of cutting the tube into loops, and step of wrapping the loops with an outer layer made of flexible material.

    Abstract translation: 制造挤压环的方法包括制备预浸纱并将纱缠绕到心轴的步骤; 将纱线固化并从形成管的纱线中取出心轴的步骤; 将管切割成环的步骤,以及用柔性材料制成的外层包裹环的步骤。

    Tubular members integrated to form a structure

    公开(公告)号:US06655633B1

    公开(公告)日:2003-12-02

    申请号:US09489041

    申请日:2000-01-21

    Abstract: Integrally stiffened and formed, load carrying structures comprising a plurality of elongated thin-walled tubes placed co-extensively in a complementary side-by-side fashion which together form a hollow structure having a desired external contour. Integral skins forming the external and internal surfaces of the structure cooperatively therewith. The structure can be formed with an underlying internal support member spanning the interior of the load carrying structure, thereby connecting opposite sides of the structure together. Also, each of the tubes are wound with fibers in controlled orientations generally paralleling the direction of the loads applied to the tubes to optimize the strength to weight ratio of the tubes.

    Method for removing mandrels from composite tubes of substantial length
    10.
    发明授权
    Method for removing mandrels from composite tubes of substantial length 失效
    从长度大的复合管中去除心轴的方法

    公开(公告)号:US5900194A

    公开(公告)日:1999-05-04

    申请号:US753646

    申请日:1996-12-27

    Applicant: Clint Ashton

    Inventor: Clint Ashton

    CPC classification number: B29C53/821 B29C33/44 B29C37/0003

    Abstract: A method for facilitating removal of a mandrel in the manufacture of hollow composite structures. A mandrel of substantially constant diameter is selected having a composition and coefficient of thermal expansion sufficient to enable it to expand when subjected to an elevated temperature. The mandrel is preheated to at least a predetermined minimum elevated temperature to thereby expand the mandrel radially outwardly. Composite material is wound around the mandrel while the mandrel has a temperature of at least the predetermined minimum elevated temperature. The composite material is then cured using any suitable curing technique. When the composite material has been cured, the mandrel is cooled to contract the mandrel radially inwardly, and the mandrel is removed from the composite material. This method of manufacture and removal is so effective that mandrels of constant diameter have been removed by hand from composite tubes of thirty feet in length.

    Abstract translation: 一种用于在中空复合结构的制造中有助于去除心轴的方法。 选择具有基本恒定直径的心轴,其具有足够的组成和热膨胀系数以使其在经受升高的温度时能够膨胀。 心轴被预热到至少预定的最小升高温度,从而使心轴径向向外膨胀。 复合材料围绕心轴缠绕,而心轴具有至少预定的最小升高温度的温度。 然后使用任何合适的固化技术固化复合材料。 当复合材料已经固化时,心轴被冷却以使心轴径向向内收缩,心轴从复合材料中移出。 这种制造和拆卸的方法如此有效,使得用三分之一长度的复合管用手去除恒定直径的心轴。

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